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REG NASA-LLIS-0394-1995 Lessons Learned - Voyager Scan Platform Problems.pdf 3

REG NASA-LLIS-0394-1995 Lessons Learned - Voyager Scan Platform Problems.pdfREG NASA-LLIS-0394-1995 Lessons Learned - Voyager Scan Platform Problems.pdf

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REG NASA-LLIS-0106-1992 Lessons Learned - Radiographic Inspections.pdf 2

REG NASA-LLIS-0106-1992 Lessons Learned - Radiographic Inspections.pdfREG NASA-LLIS-0106-1992 Lessons Learned - Radiographic Inspections.pdf

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REG NASA-LLIS-0105-1992 Lessons Learned - OMS Engine Nozzle Cover.pdf 2

REG NASA-LLIS-0105-1992 Lessons Learned - OMS Engine Nozzle Cover.pdfREG NASA-LLIS-0105-1992 Lessons Learned - OMS Engine Nozzle Cover.pdf

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REG NASA-LLIS-0104-1992 Lessons Learned - Pressure System Maintenance.pdf 2

REG NASA-LLIS-0104-1992 Lessons Learned - Pressure System Maintenance.pdfREG NASA-LLIS-0104-1992 Lessons Learned - Pressure System Maintenance.pdf

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REG NASA-LLIS-0103-1992 Lessons Learned - Draeger Pump.pdf 2

REG NASA-LLIS-0103-1992 Lessons Learned - Draeger Pump.pdfREG NASA-LLIS-0103-1992 Lessons Learned - Draeger Pump.pdf

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REG NASA-LLIS-0102-1992 Lessons Learned - High Pressure Shutoff Valves Vacuum Pump Isolation Valve.pdf 2

REG NASA-LLIS-0102-1992 Lessons Learned - High Pressure Shutoff Valves Vacuum Pump Isolation Valve.pdfREG NASA-LLIS-0102-1992 Lessons Learned - High Pressure Shutoff Valves Vacuum Pump Isolation Valve.pdf

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REG NACA-RM-A9L01-1950 Wing-tunnel investigation at Mach numbers from 0 50 to 1 29 of an all-movable triangular wing of aspect ratio 4 alone and with a body.pdf 46

REG NACA-RM-A9L01-1950 Wing-tunnel investigation at Mach numbers from 0 50 to 1 29 of an all-movable triangular wing of aspect ratio 4 alone and with a body.pdfREG NACA-RM-A9L01-1950 Wing-tunnel investigation at Mach numbers from 0 50 to 1 29 of an all-movable triangular wing of aspect ratio 4 alone and with a body.pdf

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REG NACA-RM-A9K01-1950 An analysis of the forces and pressure distribution on a wing with the leading edge swept back 37 25 degrees.pdf 104

REG NACA-RM-A9K01-1950 An analysis of the forces and pressure distribution on a wing with the leading edge swept back 37 25 degrees.pdfREG NACA-RM-A9K01-1950 An analysis of the forces and pressure distribution on a wing with the leading edge swept back 37 25 degrees.pdf

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REG NACA-RM-A9D05-1949 Wind-tunnel investigation of horizontal tails V 45 degree swept-back plan form of aspect ratio 2.pdf 46

REG NACA-RM-A9D05-1949 Wind-tunnel investigation of horizontal tails V 45 degree swept-back plan form of aspect ratio 2.pdfREG NACA-RM-A9D05-1949 Wind-tunnel investigation of horizontal tails V 45 degree swept-back plan form of aspect ratio 2.pdf

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REG NACA-RM-A8D20-1948 Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees subsonic Mach and Reynolds number effects on the characteristics of n.pdf 58

REG NACA-RM-A8D20-1948 Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees subsonic Mach and Reynolds number effects on the characteristics of n.pdfREG NACA-RM-A8D20-1948 Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees subsonic Mach and Reynolds number effects on the characteristics of n.pdf

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